JASC 2700

Service difficulty reports · 1,745

Reports filed under 2700 · Flight Control System, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '2700'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR GQRR2014FA0000674Bearing · wornLEVER BEARING WORN.Nov 11, 2014 · Boeing 737SDR GQRR2014FA0000672Bearing · wornELASTOMERIC BEARING WORN.Nov 11, 2014 · Boeing 737SDR GQRR2014FA0000676Bearing · wornELASTOMERIC BEARING WORN.Nov 10, 2014 · N7222B · Beech J35SDR AALA20141110006Unknown · malfunctionedEMERGENCY DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CLIMB RECEIVED A SLAT OVERSPEED WARNING & DISAGREE LIGHT ILLUMINATED WHILE ACCELERATING THROUGH 280 KNOTS. AUTOPILOT WOULD NOT HOLD ATTITUDE. FLIGHT CONTROLS WERE VERY HEAVY WHEN AUTOPILOTNov 10, 2014 · N555AN · Doug DC982SDR SWIA201439733Unknown · vibrationRETURNED TO THE FIELD DUE TO CREW REPORTED VIBRATIONS INFLIGHT. FELT IN THE AIRFRAME AND YOKE. PILOT SAYS THEY WERE VERY AGGRESIVE 200 AGL AND ABOVE 270 KTS. INSPECTED ACFT FLIGHT CONTROLS NO DEFECTS NOTED. RESEALED FWD MLG FAIRING FWD EDGE IAW AMM AND Nov 1, 2014 · N943SW · Cndair CL6002B19SDR SWIA201439569Unknown · unknownROLLS TO THE RIGHT DURING APPROACH. MAINTENANCE INSPECTED ALL FLIGHT CONTROLS, FAIRINGS & SURFACES. FOUND & REMOVED HIGH AERODYNAMIC SEALANT ON RT WING FLAP ACCESS PANELS.Oct 18, 2014 · N941SW · Cndair CL6002B19SDR GQRR2014FA0000675Bearing · wornELASTOMERIC BEARING WORN.Oct 11, 2014 · N7222B · Beech J35SDR OWFR2014FA0000629Guide · chafedSPRINGS FOUND CHAFING INTO SPRING GUIDES ENOUGH TO PROHIBIT PROPER CABLE TENSION ADJUSTMENT. THIS DISCREPANCY OCCURRED UNDER NORMAL WEAR AND UTILIZATION. WALL THICKNESS OF SPRING GUIDE IS .063. DEEPEST GROOVE IS .014 OF DAMAGE.Oct 10, 2014 · N426XJ · Saab 340BSDR USAA2014092900024Computer · faultedAFTER TAKEOFF CREW RECEIVED A FLIGHT CONTROL ELAC 2 PITCH FAULT ON ECAM. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. R & R NR 2 ELAC IAW AMM 27-93-34-00-001-A 400-001-A. OPERATIONS CHECKED GOOD IAW AMM 27-093-00-710-001-A.Sep 27, 2014 · N709UW · Airbus A319112SDR 2014FA0000559Control Cable · frayedTRIM CABLE FRAY AND BROKEN, STRANS AT TRIM BARREL AT STABILIZER.Sep 25, 2014 · N5114L · Piper PA28180SDR VQI2014F00030Computer · malfunctionedDURING DESCENT, ACTUATOR PITCHED UP DRAMATICALLY ON APE 2 BETWEEN 30K FT. AND 25K FT. FAULT WAS ISOLATED TO ADD 2 AND ADR 2 WAS PLACED ON MEL. OUTBID FLIGHT HAD A 1:23 MIN DELAY. TROUBLESHOOTING AND RESOLUTION DOCUMENTED BELOW; ITS YAW AS 34-44-02, AIRS SESep 23, 2014 · N840VA · Airbus A320214SDR USAA2014090200023Computer · unserviceableFLIGHT CONTROL ELAC 2 PITCH FAULT. REPLACED ELAC 2 IAW AMM 27-93-34-040-100.Sep 1, 2014 · N553UW · Airbus A321231SDR CA151125003Lever · unsecure(CAN) THE AIRCRAFT WAS ON AN ACTIVE FIRE AND WAS DISPATCHED IN THE MORNING. DURING THE FIRST SCOOP THE CREW EXPERIENCED STIFF OR BINDING POWER LEVERS WHICH PREVENTED THE AIRCRAFT REACHING MAX POWER. THE CREW HOWEVER WAS ABLE TO FORCE THE LEVERS FORWARD AND TAKAug 15, 2014 · Cndair CL2156B11215SDR HALA2014081100111Transducer · malfunctionedSENSOR FAULT ECAM UPON ADVANCING THRUST ON T/O. REMOVED SIDE STICK ASSY ON FO'S SIDE IAW AMM 27-92. R & R SIDE STICK TRASDUCER UNIT 4CE2 IAW AMM 27-92. REINSTALLED F/O'S SIDE STICK ASSY IAW AMM 27-92. ALL TEST OPS CHECK GOOD.Aug 11, 2014 · N392HA · Airbus A330243SDR ASOA20140810093Actuator · looseDURING FLIGHT, CREW FELT LIGHT VIBRATION IN THE FLIGHT CONTROLS DURING FLIGHT AND RETURNED TO BASE. ACFT WAS FERRIED, WHERE MAINTENANCE PERFORMED CABLE TENSIONS AND FUNCTIONAL TEST OF THE AILERON, RUDDER AND ELEVATOR, FOUND THE AILERON CABLE SLIGHTLY OUT OF Aug 10, 2014 · N14960 · Emb EMB145LRSDR SOKF20140812006Computer · faultyDURING CLIMB THE ACFT RETURNED DUE ELAC 2 FAULT. IAW TSM 27-93-00-810-967-A PERFORMED R & R OF ELAC 2 IAW AMM 27-93-34-000-001 & AMM 27-93-34-400-001. PERFORMED OPERATIONAL TEST IAW AMM 27-93-00-710-001 & LAND CAT III CAPABILITY TEST IAW AMM TASK 22-97-00-71Aug 8, 2014 · N493TA · Airbus A320233SDR YENA20140618112Secu · failedCREW DECLARED AN EMERGENCY, FLIGHT CONTROL AILERON SERVO FAULT UNCOMMANDED PITCH, AILERON FLUTTER. PERFORMED TSM 27-10-00-810-824A AND TSM 27-93-00-810-918A. R & R NR 1 ELAC AND NR 2 SEC WORKED IAW 27-93-34 AND 27-94-34. PERFORMED OPS TEST OF ELAC'S AND SECJun 18, 2014 · N779JB · Airbus A320232SDR YENA20140618111Computer · failedCREW DECLARED AN EMERGENCY, FLIGHT CONTOL AILERON SERVO FAULT UNCOMMANDED PITCH, AILERON FLUTTER. PERFORMED TSM 27-10-00-810-824A AND TSM 27-93-00-810-918A. R & R NR 1 ELAC AND NR 2 SEC WORKED IAW 27-93-34 AND 27-94-34. PERFORMED OPS TEST OF ELAC'S AND SEC'Jun 18, 2014 · N779JB · Airbus A320232SDR F3LA2014061601043Computer · failedUPON THRUST REDUCTION AFTER TAKEOFF ACFT ENTERED ALT LAW & END. R & R NR 1 ELAC. OPERATIONS TESTED GOOD IAW MM 278-93-34 PB 401. PERFORMED LAND CAT 3 CAPABILITY TEST. OPERATIONS TESTED GOOD IAW AMM 22-97-00-710-001. ACFT RETAINS CAT IIIB STATUS.Jun 13, 2014 · N221FR · Airbus A320214SDR SWIA2014051637607Pcu · malfunctionedAIRCRAFT ROLLED TO RT. REPLACED INBD AND OTBD MFS PCU'S.May 15, 2014 · N824SK · Cndair CL6002D24SDR CALA2014050690959Handle · defectiveCAPTAIN'S PTT ON STICK CONSTANTLY TRANSMITS. REPLACED CAPTAIN'S SIDE STICK HANDLE IAW AMM 27-92-91. PTT OPERATIONS TEST OK IAW AMM 23-12-00. PRIORITY TEST OK IAW AMM 27-96-00. SIDE STICK OPERATIONS TEST OK IAW AMM 27-92-41.May 3, 2014 · N452UA · Airbus A320232SDR 2014FA0000329Grip · failedDURING THE ON SCENE INVESTIGATION OF LANDING INCIDENT WHICH OCCURRED DURING A LANDING WITH SLIGHT LT CROSSWIND, THE PILOT LOST CONTROL OF ACFT APPROX 10 FT AGL WHEN FOAM GRIP ON CONTROL STICK CAME OFF THE CONTROL STICK. ACFT IMMEDIATELY DROPPED THE RT WING, LMay 2, 2014 · N2598G · Bbavia 7ECASDR J6MR2014FA0000355Valve · intermittentSTABILIZER MISCOMPARE REPORTED BY CREW ON APPROACH. FOUND STABILIZER ACTUATOR VY013 INTERMITTENT. REPLACED UNIT.Apr 27, 2014 · N39RC · Cessna 560XLSDR CA140430006Control Wheel · cracked(CAN) THE CONTROL WHEEL WAS FOUND CRACKED THOUGH A NARROW SECTION OF THE BOTTOM OF THE WHEEL FROM THE MAP LIGHT HOLE TO THE FRONT EDGE OF THE CASTING. THE CRACK WEAKENS THE CONTROL WHEEL STRUCTURE AND IS LIKELY CAUSED BY NORMAL ELEVATOR-UP COMMAND INPUTS.Apr 16, 2014 · Cessna 172SSDR VNAA2014041300012Unknown · malfunctionedCREW REPORTED UNCOMMANDED YAW AFTER TAKEOFF. RUDDER TRIM REQUIRED TO MAINTAIN CONTROL. RUDDER TRIM WAS TURNING TOWARDS FULL LEFT. CREW DECLARED EMERGENCY, DIVERTED AND LANDED SAFELY. PERFORMED OPS TEST OF RUDDER CONTROL SYS IAW AMM 27.21.00.710.801. OPS CHEApr 13, 2014 · N228PS · Cndair CL6002B19SDR SWIA201437066Flt Controls · malfunctionedAT ABOUT 1000 FEET AGL DURING FINAL, ACFT WANTED TO ROLL TO THE LEFT. POWER SETTINGS MATCHED. FLAPS WERE SELECTED TO 45 DEGREES. REQUIRED QUITE A BIT OF RT AILERON ALL THE WAY TO THE GROUND. INSPECTED AND CLEANED LT AND RT FLAPS. SANDED ROUGH PAINT ON LT INApr 9, 2014 · N959SW · Cndair CL6002B19SDR CALA2014041090792Computer · faultySEVERE VIBRATION IN TAIL AT .76 AT FL240 IN CLIMB. ALL INDICATIONS NORMAL IAW SURVEY 05-50-00-810-8 01A. FOUND TO BE IN TAIL SECTION, PANEL 344DB RT ELEVATOR ACTUATOR PANEL LOOSE. PERFORMED ELEVATOR OSCILLATION TEST IAW 27-34-00, FOUND .005 - .008 ON BOTH SApr 9, 2014 · N812UA · Airbus A319131SDR DXTA2014040405715Unknown · vibrationVIBRATION BEGINS AT FL260 AT 290KTS, INCREASED INTENSITY TO 350KTS. FELT IN CONTROL COLUMN & NOT IN RUDDER PEDALS. VIBRATION FELT IN COCKPIT SEATS & IN CABIN SEATS. CHECKED ALL ELEVATOR BELLCRANKS, PUSHRODS, CONTROL COLUMS AND HINGE POINTS FOR CONDITION ANDMar 29, 2014 · N707QS · Gulstm 200SDR CALA2014030390518Module · faultyMACH SPEED TRIM EICAS ON. REPLACED RT SAM MODULE IAW AMM 27-09-00, PG 201, CHECKED OK.Feb 28, 2014 · N597UA · Boeing 757222SDR USAA2014022400003Unknown · malfunctionedWHEN SPOILERS EXTENDED ACFT ROLLED TO THE RT. ON FLIGHT CONTROL PAGE ALL EXTENDED AT THE SAME TIME. PERFORMED OPERATIONS TEST OF THE SPOILER ACTUATORS IAW AMM 27-64-00-710-0014. OPERATIONS TESTED GOOD, NO HISTORY.Feb 22, 2014 · N654AW · Airbus A320232SDR CALA2014022190414Unknown · malfunctionedALTERNATE LAW PROT LOST DISPLAYED ON UPPER ECAM SCREEN, FLIGHT CONTROL. CYCLED BREAKERS B 3 & 4. PERFORMED AFS TEST IAW MM22-96-00, CHECKED GOOD.Feb 19, 2014 · N409UA · Airbus A320232SDR CALA2014021790395Unknown · malfunctionedUNCOMMANDED YAW LT & RT ON CLIMB.Feb 14, 2014 · N562UA · Boeing 757222SDR CALA2014012890258Computer · faultedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN.Jan 25, 2014 · N417UA · Airbus A320232SDR CA140120007Computer · failed(CAN) FLIGHT DEPARTED AND BEGAN TO EXPERIENCE AN AIRFRAME VIBRATION, CREW DECLARED A PAN PAN AND DIVERTED BACK. EMERGENCY CREWS WERE ON STAND BY ON LANDING AND ONCE ON GROUND WERE WAIVED OFF BY FLIGHT. R & R ELAC NR 1 IAW AMM 27-93-24 PB401. PERFORMED OPS TJan 18, 2014 · Airbus A321211SDR DALA1515940907Jackscrew · not reportedHORIZONTAL STABILIZER JACKSCREW REPAIRED IAW AA 2740-01113.Dec 31, 2013 · N907DL · Doug MD88SDR CALA2013123194067Computer · faultedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. GOT ECAM WHEN NR 1 GENERATOR CAME ONLINE. CYCLED ELAC 1 IAW FM. ACCOMPLISH CHRONIC REVIEW. ITEM ROLLED FORWARD. ELAC 1 PITCH FAULT. IAW DF 2793A.Dec 30, 2013 · N419UA · Airbus A320232SDR CALA2013123094017Unknown · malfunctionedEQ4040 PRIMARY FLT CONTROL TEST FAILED, MESSAGE 27-10308. FLAPERON POWER CONTROL UNIT LT INBD ACTUATION CONFIDENCE TEST FAILED SEVERAL TIMES. RESET K26 CB & POWER SUPPLY CB ON 5E RACK, NO HELP. SWAPPED THE ACE WITH ANOTHER, NO HELP. SWAPPED THE ACE TO ORIGDec 30, 2013 · N219UA · Boeing 777222SDR CALA2013122793969Flt Controls · vibrationCREW REPORT HIGH SPEED AIRFRAME VIBRATION, IAW TO LOG01 AIRCRAFT VIBRATION. BEGAN TROUBLESHOOTING IAW FELT ON RUDDER PEDALS & REPORTED AS MODERATE IN AFT CABIN. 320 IAW AMM 27-24-00 PG 3 OF 12 UP TO ITEM B, NEED CONT FROM HERE THRU TO END.Dec 27, 2013 · N493UA · Airbus A320232SDR CALA2013122393884Computer · faultySEC 2 FAULT RECURRING. WILL RESET FOR A FEW MINUTES THEN TRIPS. REPLACED SEC 2 COMPUTER IAW AMM 27-94-34-000-001-A & 27-94-34-400-001-A. PASSED OPERATIONAL TESTS IAW AMM 27-94-00-710-003 27-94-00-710-003-A. ECAM MESSAGE CLEARED.Dec 21, 2013 · N496UA · Airbus A320232SDR CALA2013121693749Computer · faultySEC 1 FAULT, REPLACED SEC 1 WITH SEC 3 IAW MM. SEC 1 NOW MR 27997-137, SEC 3 NOW MR27997-1120. SEC 3 NOW INOPERATIVE & DEFERRED IAW MEL 2794A.Dec 15, 2013 · N494UA · Airbus A320232SDR CALA2013121693745Computer · faultySIDE STICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN F CTL. REPLACED NR 1 ELAC, OPERATIONS TESTED OKAY.Dec 15, 2013 · N480UA · Airbus A320232SDR CALA2013121693729Computer · faultySEC 1 ECAM MSG SHOWN. REPLACED COMPUTER. REPLACED SEC 1 COMPUTER IAW MM & ACCOMPLISHED OPERATIONS CHECK IAW MM, CHECKED OK. CORRECT OPERATIONS CHECK IAW TO 27-94-00-710-002-ADec 14, 2013 · N419UA · Airbus A320232SDR CALA2013121693702Accelerometer · faultySEC 1 FAIL AFTER START. QRH RESET ON GROUND, NO HELP. TURNED OFF ALL HYDS SWITCH IAW TOM. IAW POST FLIGHT REPORT & AMIS HISTORY, REPLACED ACCELEROMETER 12CE2, IAW AMM 27-92-16-4 01. TEST PASSED, SEC 1 TEST PASSED IAW AMM 27-94-00-501.Dec 13, 2013 · N417UA · Airbus A320232SDR RAIA201312070003Unknown · unknownCONTROLS FEEL LIKE THEY ARE CATCHING TO THE LEFT, AND TO HOLD A LOT OF LEFT AILERON ON APPROACH, HAVE OVER 50 PERCENT RT AILERON TRIM SET. MAINTENANCE R & R AILERON SERVO, NO FIX.Dec 7, 2013 · N805HK · Emb EMB145EPSDR CALA2013120393405Computer · faultyAIL SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. FCTL AIL SERVO FAULT IMMEDIATELY AFTER TAKEOFF. REPLACED ELAC 1, OPERATIONAL TEST OF ELAC PASSED.Nov 30, 2013 · N488UA · Airbus A320232SDR FGQR2014FA0000007Cable · frayedROLL SERVO CABLE ASSY FOUND FRAYED & UNRAVELED AT LOWER IDLER PULLEY. FURTHER INVESTIGATION FOUND FRAYING STARTING AT UPPER IDLER PULLEY. ALSO, PULLEYS LOCATED AT RT WS 154.Nov 27, 2013 · N206BR · Cessna U206GSDR CALA2013112293193Computer · faultyFLIGHT CONTROL ELEV SERVO FAULT DURING FLIGHT CONTROL CHECK ON TAXI OUT. REPLACED ELAC 2 IAW AMM 27-93-34 ACP CAT III TEST FULL AUTO LAND CAPABLE.Nov 21, 2013 · N419UA · Airbus A320232SDR CALA2013112093096Computer · faultyDUE TO HISTORY ELAC 2 NEEDS R & R. REPLACED ELAC, OPERATIONS CHECKED NORMAL.Nov 17, 2013 · N478UA · Airbus A320232SDR CALA2013111292837Cover · missingDISK COVER FOR BOLT OTBD CTR FLAP PYLON MISSING NEAR R4 MAG FUEL LEVEL.Nov 11, 2013 · N488UA · Airbus A320232SDR CALA2013110892759Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, F CTL. ELAC 2 FAULT HAPPEN WHEN AUTOPILOT ENGAGED RESETS WITH AP OFF BUT FAULTS AGAIN W AP PROG TEXT. ACCOMPLISHED CHRONIC REVIEW. R & R ELAC 2 COMPUTER IAW AMM 27-93-34-400-001 OPERATIONS CHECKED GOOD. UNABLE TNov 7, 2013 · N810UA · Airbus A319131
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